Advanced Propulsion Systems

Hypersonic flight is a heat problem long before it is a speed problem. Sustained travel above Mach 5 puts leading edges and inlets into a thermal regime where most materials stop behaving predictably, which is why so many programs stall at the same point in testing.

This section follows propulsion that has not entered service. Adaptive-cycle engines, scramjets and ramjets, combined-cycle concepts, solid rocket motor chemistry and casting capacity, electric and hybrid work for unmanned aircraft.

Test campaigns are reported with their conditions attached. A flight at Mach 5 held for two hundred seconds is a different result from a captive-carry demonstration, and both get described as what they were. Engines already in production are a separate subject.

Related Coverage

Aircraft Propulsion covers engines already in production and in service, which is the harder boundary to hold in hypersonics reporting. The airframes and weapons these concepts are meant to power sit in Missiles / Drones / Directed Energy and Aircraft.

Weapons & Technologies is the parent section. Solid rocket motor capacity, castings and the single-source supplier problem are in Defense Infrastructure & Manufacturing. Launch propulsion appears again in Space Systems. Reports & Analysis carries the technology-readiness assessments, which tend to be less optimistic than program briefings.